|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
9:1
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:competitors
|
gptkb:CF34
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:customer_support
|
gptkb:Air_Canada
|
|
gptkbp:design
|
high bypass ratio
|
|
gptkbp:development
|
gptkb:GTF_engine_family
|
|
gptkbp:diameter
|
1,600 mm
1,500 mm
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:Geared_Turbofan
advanced materials
state-of-the-art technology
mass production
various aircraft models
global support network
final assembly line
future upgrades planned
|
|
gptkbp:engine_configuration
|
modular design
twin-engine
detailed specifications available.
|
|
gptkbp:engine_delivery
|
on-time delivery
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_type
|
gptkb:PW1500_G
gptkb:jet_engine
|
|
gptkbp:first_flight
|
gptkb:2013
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1200 G-14
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_use
|
gptkb:2016
|
|
gptkbp:propulsion
|
18,000 lbf
20,000 lbf
5.56
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
geared turbofan
|
|
gptkbp:used_in
|
gptkb:Bombardier_CSeries
|
|
gptkbp:weight
|
3,600 lb
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW1200_G
|
|
gptkbp:bfsLayer
|
6
|